
%
% Helicopter
%

A=[    0        1        0       0        0       0 ;
   -0.80435   -0.1    0.80435    0     48.261     0 ;
       0        0        0       1        0       0 ;
    1.6086      0     -1.6087    0        0       0 ;
       0        0        0       0        0       1 ;
       0       0.5       0       0        0      -2 ]
B=[0;
   0;
   0;
   0;
   0;
   1]
